A generalized approach to decompose the compressible Navier-Stokes equations into an equivalent set of coupled equations for flow and acoustics is introduced. As a significant extension to standard hydrodynamic/acoustic splitting methods, the approach provides the essential coupling terms, which account for the feedback from the acoustics to the flow. A unique simplified version of the split equation system with feedback is derived that conforms to the compressible Navier-Stokes equations in the subsonic flow regime, where the feedback reduces to one additional term in the flow momentum equation. Subsonic simulations are conducted for flow-acoustic feedback cases using a scale-resolving runtime coupled hierarchical Cartesian mesh solver, ...
AbstractAn aerodynamic sound source extraction from a general flow field is applied to a number of m...
In the present paper an Expansion about Incompressible Flow approach, as suggested by Shen and Søren...
Abstract. In the present paper an Expansion about Incompressible Flow approach, as suggested by Shen...
Hybrid computational aeroacoustics applications approaches, in which the computational domain is spl...
Different strategies regarding the simulation of sound generation and propagation are explored. A hy...
In computational acoustics, fluid-acoustic coupling methods for the computation of sound have been w...
This thesis involves the computation of aerodynamically generated sound using a source-extraction ba...
The Expansion about Incompressible Flow (EIF) approach is a computational aeroacoustics (CAA) techni...
An aero-acoustic coupling method based on the splitting into noise sources generation and acoustic p...
Hybrid CAA-approaches are commonly used for aero-acoustic engineering applications. For these kinds ...
An explicit time/space finite difference procedure is used to model the propagation of sound in a qu...
The computation of flow-induced noise at low Mach numbers usually relies on a two-step hybrid method...
Computational aeroacoustics deals with the computation of noise generated arodynamically. In order t...
International audienceA pressure-correction algorithm is presented for compressible fluid flow regim...
This contribution deals with the acoustic simulation of aerodynamical noise generated by a flow over...
AbstractAn aerodynamic sound source extraction from a general flow field is applied to a number of m...
In the present paper an Expansion about Incompressible Flow approach, as suggested by Shen and Søren...
Abstract. In the present paper an Expansion about Incompressible Flow approach, as suggested by Shen...
Hybrid computational aeroacoustics applications approaches, in which the computational domain is spl...
Different strategies regarding the simulation of sound generation and propagation are explored. A hy...
In computational acoustics, fluid-acoustic coupling methods for the computation of sound have been w...
This thesis involves the computation of aerodynamically generated sound using a source-extraction ba...
The Expansion about Incompressible Flow (EIF) approach is a computational aeroacoustics (CAA) techni...
An aero-acoustic coupling method based on the splitting into noise sources generation and acoustic p...
Hybrid CAA-approaches are commonly used for aero-acoustic engineering applications. For these kinds ...
An explicit time/space finite difference procedure is used to model the propagation of sound in a qu...
The computation of flow-induced noise at low Mach numbers usually relies on a two-step hybrid method...
Computational aeroacoustics deals with the computation of noise generated arodynamically. In order t...
International audienceA pressure-correction algorithm is presented for compressible fluid flow regim...
This contribution deals with the acoustic simulation of aerodynamical noise generated by a flow over...
AbstractAn aerodynamic sound source extraction from a general flow field is applied to a number of m...
In the present paper an Expansion about Incompressible Flow approach, as suggested by Shen and Søren...
Abstract. In the present paper an Expansion about Incompressible Flow approach, as suggested by Shen...